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JNTU 2007-2008 III YEAR II SEM. B. TECH. AE - FLIGHT VEHICLE DESIGN

Posted Date: 09 Dec 2007 Resource Type: Articles/Knowledge Sharing Category: Syllabus

Posted By: Sri Member Level: Gold
Rating:

Points: 1

JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY
HYDERABAD
III Year B. Tech. AE – II semester T P C
4+1* 0 4
FLIGHT VEHICLE DESIGN

UNIT-I
OBJECTIVES REQUIREMENTS OF THE VEHICLE : Type, role, mission. Payload, performance and other requirements. Study of comparable aircraft - principal design and constructional and performance. Data collection and statistical analysis.

UNIT-II
CONCEPTUAL SKETCH AND FIRST ESTIMATE OF WEIGHT : Conceptual sketch of candidate design- alternative configurations. First estimate of take off weight.

UNIT-III
INITIAL SIZING : Airfoil and wing geometry selection. Estimate of thrust to weight ratio and wing loading.

UNIT-IV
FUSELAGE AND CONTROL SURFACES : Sizing of Fuselage and control surfaces.

UNIT-V
CONFIGURATION LAYOUT : Layout and drawing of the configuration. Weightbalance

UNIT-VI
PERFORMANCE AND STABILITY ESTIMATE : Performance and stability estimate.

UNIT-VII
LOAD ESTIMATES : Airload distribution on the wing. Preliminary structural Layout.

UNIT-VIII
REVIEW : Review and evaluation of the design.

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